US2018156099A1PendingUtilityA1

Method of measuring an exhaust gas temperature

Assignee: GM GLOBAL TECH OPERATIONS LLCPriority: Dec 6, 2016Filed: Dec 6, 2016Published: Jun 7, 2018
Est. expiryDec 6, 2036(~10.4 yrs left)· nominal 20-yr term from priority
F01N 2610/03F01N 3/2066F01N 3/206F01N 2610/1453B01D 53/944F01N 2610/148F01N 11/005F01N 2610/02B01D 53/9431F01N 3/2033Y02T10/12F01N 2900/0406F01N 2900/1411B01D 53/9495F01N 2560/06F01N 2900/1404Y02T10/40B01D 53/9477
32
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Claims

Abstract

A method of measuring exhaust gas temperatures in an exhaust pipe of an internal combustion engine is disclosed. A value of a mass flow rate of exhaust gasses flowing into the exhaust pipe is determined. A signal yielded by a temperature sensor located in a first point of the exhaust pipe is sampled and applied as input to a first computational module that yields a corresponding first output signal. A value of the temperature of the exhaust gasses flowing in the first point of the exhaust pipe is calculated on the basis of a value of the first output signal.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . A method of measuring exhaust gas temperatures in an exhaust pipe of an internal combustion engine comprising:
 determining a value of a mass flow rate of exhaust gasses flowing into the exhaust pipe;   sampling a signal yielded by a temperature sensor located in a first point of the exhaust pipe;   applying the signal as input to a first computational module that yields a corresponding first output signal, wherein the first computational module has the following transfer function:
     F *( s )=(1+τ RT   ·s )· F ( s )
 
   calculating a value of the temperature of the exhaust gasses flowing in the first point of the exhaust pipe on the basis of the first output signal; and   wherein F(s) is the signal yielded by the temperature sensor, F*(s) is the first output signal and τ RT  is a coefficient determined as a function of the measured value of the mass flow rate of exhaust gasses.   
     
     
         2 . The method according to  claim 1 , wherein the first computational module implements the following equation:
     f *( t )= f ( t )+τ RT   ·f ′( t )
   wherein f(t) is a value of the signal sampled at a time t, f*(t) is a value of the first output signal at the time t, and f′(t) is a value of a derivative of the signal at the time t.   
     
     
         3 . The method according to  claim 2 , further comprising calculating the value f′(t) of the derivative of the signal with a finite difference equation. 
     
     
         4 . The method according to  claim 3 , wherein the calculation of the value f′(t) of the derivative of the signal is performed with the following finite difference equation: 
       
         
           
             
               
                 
                   f 
                   ′ 
                 
                  
                 
                   ( 
                   t 
                   ) 
                 
               
               = 
               
                 
                   1 
                   T 
                 
                 · 
                 
                   
                     ∑ 
                     
                       k 
                       = 
                       0 
                     
                     n 
                   
                    
                   
                     
                       C 
                       k 
                     
                     · 
                     
                       f 
                        
                       
                         ( 
                         
                           t 
                           - 
                           kT 
                         
                         ) 
                       
                     
                   
                 
               
             
           
         
         wherein T is a sampling period of the signal, f(t−kT) is a value of the signal sampled at the time t−kT, C k  is a predetermined coefficient and n is a predetermined positive real number. 
       
     
     
         5 . The method according to  claim 4 , wherein T is equal to 0.1 seconds, n is equal to 3, C 0  is equal to 11/6, C 1  is equal to 3, C 2  is equal to 3/2 and C 3  is equal to ⅓. 
     
     
         6 . The method according to  claim 1 , further comprising:
 applying the first output signal to a second computational module that yields a corresponding second output signal, wherein the second computational module has the following transfer function:   
       
         
           
             
               
                 
                   F 
                   ** 
                 
                  
                 
                   ( 
                   s 
                   ) 
                 
               
               = 
               
                 
                   1 
                   
                     1 
                     + 
                     
                       
                         τ 
                         TC 
                       
                       · 
                       s 
                     
                   
                 
                 · 
                 
                   
                     F 
                     * 
                   
                    
                   
                     ( 
                     s 
                     ) 
                   
                 
               
             
           
         
         calculating the value of the temperature of the exhaust gasses flowing in the first point of the exhaust pipe on the basis of a value of the second output signal; 
         wherein F**(s) is the second output signal and τ TC  is a coefficient determined as a function of the measured value of the mass flow rate of exhaust gasses, 
       
     
     
         7 . The method according to  claim 6 , wherein the second computational module implements the following equation: 
       
         
           
             
               
                 
                   f 
                   ** 
                 
                  
                 
                   ( 
                   t 
                   ) 
                 
               
               = 
               
                 K 
                 · 
                 
                   ( 
                   
                     1 
                     - 
                     
                       e 
                       
                         
                           - 
                           t 
                         
                         
                           τ 
                           TC 
                         
                       
                     
                   
                   ) 
                 
                 · 
                 
                   
                     f 
                     * 
                   
                    
                   
                     ( 
                     t 
                     ) 
                   
                 
               
             
           
         
         wherein f*(t) is a value of the first output signal at a time t, f**(t) is a value of the second output signal at the time t and K is a coefficient. 
       
     
     
         8 . The method according to  claim 6 , wherein the second computational module implements the following equation:
     f **( t )= f *( t )· K   TC   +f **( t−T )·(1− K   TC )
   wherein f*(t) is a value of the first output signal at a time t, f**(t) is a value of the second output signal at the time t, K TC  is a coefficient determined as a function of the measured value of the flow rate of exhaust gasses, and T is a sampling period of the signal.   
     
     
         9 . The method according to  claim 1 , further comprising estimating a value of a temperature of the exhaust gasses flowing in a second different point (P 2 ) of the exhaust pipe ( 275 ) on the basis of the calculated value of the temperature of the exhaust gasses in the first point (P 1 ). 
     
     
         10 . The method according to  claim 9 , wherein the value of the temperature of the exhaust gasses flowing in the second point of the exhaust pipe is calculated with the following equation: 
       
         
           
             
               
                 
                   
                     T 
                     1 
                   
                   · 
                   
                     
                       m 
                       . 
                     
                     g 
                   
                   · 
                   
                     c 
                     
                       p 
                       g 
                     
                   
                 
                 + 
                 
                   
                     T 
                     u 
                   
                   · 
                   
                     
                       m 
                       . 
                     
                     u 
                   
                   · 
                   
                     c 
                     
                       p 
                       u 
                     
                   
                 
                 + 
                 
                   
                     T 
                     2 
                   
                   · 
                   
                     ( 
                     
                       
                         
                           
                             m 
                             . 
                           
                           g 
                         
                         · 
                         
                           c 
                           
                             p 
                             g 
                           
                         
                       
                       + 
                       
                         
                           
                             m 
                             . 
                           
                           u 
                         
                         · 
                         
                           c 
                           
                             p 
                             u 
                           
                         
                       
                     
                     ) 
                   
                 
                 - 
                 
                   
                     ( 
                     
                       
                         m 
                         u 
                       
                       + 
                       
                         m 
                         g 
                       
                     
                     ) 
                   
                   · 
                   
                     c 
                     
                       p 
                       m 
                     
                   
                   · 
                   
                     
                       dT 
                       m 
                     
                     dt 
                   
                 
                 - 
                 
                   
                     Q 
                     . 
                   
                   mw 
                 
                 - 
                 
                   
                     
                       m 
                       . 
                     
                     u 
                   
                   · 
                   
                     k 
                     vap 
                   
                 
               
               = 
               0 
             
           
         
         wherein T 1  is a value of the temperature of the exhaust gasses flowing in a first point of the exhaust pipe, {dot over (m)} g  is the value of a mass flow rate of exhaust gasses flowing in the exhaust pipe ( 278 ), c p     g    is a specific heat capacity of the exhaust gasses, T u  is a temperature value of a fluid injected by an injector ( 279 ) located between the first and the second point of the exhaust pipe, {dot over (m)} u  is a value of a mass flow rate of the injected fluid, c p     u    is a specific heat capacity of the injected fluid, T 2  is the value of the temperature of the exhaust gasses flowing in the second point of the exhaust pipe, m u  is a value of a mass of the injected fluid in the exhaust pipe ( 278 ), m g  is a value of a mass of exhaust gasses in the exhaust pipe ( 278 ), c p     m    is a specific heat capacity of a mixture of exhaust gasses and injected fluid in the exhaust pipe ( 278 ), T m  is a mean value of the temperature of the mixture of exhaust gasses and injected fluid, {dot over (Q)} mw  is a value of a thermal flux between the exhaust pipe ( 278 ) and the mixture of exhaust gasses and injected fluid, and k vap  is a coefficient representative of an energy spent for mixing and vaporizing the injected fluid and k vap  is a coefficient representative of an energy spent for mixing and vaporizing the injected fluid. 
       
     
     
         11 . A non-transitory computer readable medium comprising a computer program for measuring exhaust gas temperatures in an exhaust pipe of an internal combustion engine, the computer program having a program code, which when run on a computer, is configured to:
 determine a value of a mass flow rate of exhaust gasses flowing into the exhaust pipe;   sample a signal yielded by a temperature sensor located in a first point of the exhaust pipe;   apply the signal as input to a first computational module that yields a corresponding first output signal, wherein the first computational module has the following transfer function:
     F *( s )=(1+τ RT   ·s )· F ( s )
 
   calculate a value of the temperature of the exhaust gasses flowing in the first point (P 1 ) of the exhaust pipe ( 275 ) on the basis of a value of the first output signal;   wherein F(s) is the signal yielded by the temperature sensor, F*(s) is the first output signal and τ RT  is a coefficient determined as a function of the measured value of the mass flow rate of exhaust gasses.   
     
     
         12 . An internal combustion engine comprising an exhaust pipe having a temperature sensor located in a first point of the exhaust pipe and an electronic control unit configured to:
 determine a value of a mass flow rate of exhaust gasses flowing into the exhaust pipe;   sample a signal yielded by the temperature sensor;   apply the signal as input to a first computational module that yields a corresponding first output signal, wherein the first computational module has the following transfer function:
     F *( s )=(1+τ RT   ·s )· F ( s )
 
   calculate a value of the temperature of the exhaust gasses flowing in the first point (P 1 ) of the exhaust pipe ( 275 ) on the basis of a value of the first output signal;   wherein F(s) is the signal yielded by the temperature sensor, F*(s) is the first output signal and τ RT  is a coefficient determined as a function of the measured value of the mass flow rate of exhaust gasses.

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